US20160090995A1 - Ejector - Google Patents

Ejector Download PDF

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Publication number
US20160090995A1
US20160090995A1 US14/890,170 US201414890170A US2016090995A1 US 20160090995 A1 US20160090995 A1 US 20160090995A1 US 201414890170 A US201414890170 A US 201414890170A US 2016090995 A1 US2016090995 A1 US 2016090995A1
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United States
Prior art keywords
refrigerant
space
swirling
swirling space
passage
Prior art date
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Abandoned
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US14/890,170
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English (en)
Inventor
Etsuhisa Yamada
Yoshiaki Takano
Haruyuki Nishijima
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Denso Corp
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Denso Corp
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Assigned to DENSO CORPORATION reassignment DENSO CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: NISHIJIMA, HARUYUKI, TAKANO, YOSHIAKI, YAMADA, ETSUHISA
Publication of US20160090995A1 publication Critical patent/US20160090995A1/en
Abandoned legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44—Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B41/00—Fluid-circulation arrangements
    • F25B41/30—Expansion means; Dispositions thereof
    • F25B41/31—Expansion valves
    • F25B41/33—Expansion valves with the valve member being actuated by the fluid pressure, e.g. by the pressure of the refrigerant
    • F25B41/335—Expansion valves with the valve member being actuated by the fluid pressure, e.g. by the pressure of the refrigerant via diaphragms
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/02—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid
    • F04F5/04—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being liquid displacing elastic fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04F—PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00—Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44—Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46—Arrangements of nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B41/00—Fluid-circulation arrangements
    • F25B41/062—
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60H—ARRANGEMENTS OF HEATING, COOLING, VENTILATING OR OTHER AIR-TREATING DEVICES SPECIALLY ADAPTED FOR PASSENGER OR GOODS SPACES OF VEHICLES
    • B60H1/00—Heating, cooling or ventilating [HVAC] devices
    • B60H1/32—Cooling devices
    • B60H2001/3286—Constructional features
    • B60H2001/3298—Ejector-type refrigerant circuits
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2327/00—Refrigeration system using an engine for driving a compressor
    • F25B2327/001—Refrigeration system using an engine for driving a compressor of the internal combustion type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2341/00—Details of ejectors not being used as compression device; Details of flow restrictors or expansion valves
    • F25B2341/001—Ejectors not being used as compression device
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2341/00—Details of ejectors not being used as compression device; Details of flow restrictors or expansion valves
    • F25B2341/001—Ejectors not being used as compression device
    • F25B2341/0012—Ejectors with the cooled primary flow at high pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2341/00—Details of ejectors not being used as compression device; Details of flow restrictors or expansion valves
    • F25B2341/06—Details of flow restrictors or expansion valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2400/00—General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
    • F25B2400/23—Separators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2500/00—Problems to be solved
    • F25B2500/18—Optimization, e.g. high integration of refrigeration components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2600/00—Control issues
    • F25B2600/02—Compressor control
    • F25B2600/025—Compressor control by controlling speed
    • F25B2600/0253—Compressor control by controlling speed with variable speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B27/00—Machines, plants or systems, using particular sources of energy
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B40/00—Subcoolers, desuperheaters or superheaters
    • F25B40/02—Subcoolers

Definitions

  • the present disclosure relates to an ejector that depressurizes a fluid, and draws the fluid by a suction action of an ejection fluid at high speed.
  • Patent Document 1 discloses a depressurizing device that is applied to a vapor compression refrigeration cycle device, and depressurizes the refrigerant.
  • the depressurizing device of Patent Document 1 has a main body that defines a swirling space in which the refrigerant is swirled, and swirls the refrigerant within the swirling space, to thereby reduce a refrigerant pressure on a swirling center side to a pressure at which the refrigerant is depressurized and boiled (cavitation occurs). Further, the depressurizing device allows the refrigerant in a gas-liquid mixing state in which a gas-phase refrigerant and a liquid-phase refrigerant on the swirling center side are mixed together to flow into a minimum passage area part for depressurization.
  • Patent Document 1 also discloses an ejector using the depressurizing device as a nozzle.
  • the ejector of this type draws the gas-phase refrigerant flowing out of the evaporator due to the suction action of the ejected refrigerant ejected from the nozzle, and mixes the ejected refrigerant with the suction refrigerant in a pressure increase part (diffuser portion), thereby being capable of increasing the pressure.
  • a refrigeration cycle device (hereinafter referred to as an ejector type refrigeration cycle) including an ejector as a refrigerant depressurization device
  • power consumption of a compressor can be reduced with the use of a refrigerant pressure increase action in the pressure increase part of an ejector, and a coefficient of performance (COP) of a cycle can be improved to a greater extent than a general refrigeration cycle device including an expansion valve or the like as the refrigerant depressurization device.
  • COP coefficient of performance
  • a variation in the ejected refrigerant ejected from the nozzle is suppressed, and the refrigerant in the gas-liquid mixing state is depressurized in the minimum passage area part to promote the boiling of the liquid-phase refrigerant and improve the nozzle efficiency.
  • the nozzle efficiency represents an energy conversion efficiency for converting a pressure energy of the refrigerant into a kinetic energy in the nozzle.
  • the present inventors have searched the cause, and found that in the ejector disclosed in Patent Document 1, the refrigerant flows into a tangential direction of the swirling space circular in cross-section when the refrigerant flows into the swirling space, and this flow makes impossible to improve the nozzle efficiency to the desired value.
  • the reason is because when the refrigerant flows in the tangential direction of the swirling space circular in cross-section, the depressurization and boiling of the refrigerant in the swirling space is limited as will be described later.
  • Patent Document 1 JP 2012-202653 A
  • it is an objective of the present disclosure is to limit a reduction in nozzle efficiency of an ejector that depressurizes a fluid which is swirled into a gas-liquid mixing state.
  • an ejector includes a swirling space formation member having a swirling space in which a fluid is swirled, a nozzle that depressurizes and ejects the fluid flowing out of the swirling space, and a body including a fluid suction port that draws a fluid due to a suction action of the ejected fluid at high speed which is ejected from the nozzle, and a pressure increase part that mixes the ejected fluid with the suction fluid drawn from the fluid suction port and increases a pressure of the mixed fluid.
  • the swirling space includes an upstream swirling space in which the fluid flowing from an external is swirled, and a downstream swirling space that introduces the fluid flowing out of the upstream swirling space into the nozzle with keeping the fluid swirling.
  • the upstream swirling space and the downstream swirling space have respective rotating body shapes in which center axes are disposed coaxially with each other.
  • the upstream swirling space has an outlet part through which the fluid outflows to the downstream swirling space, and the outlet part has an annular shape along an outer peripheral shape of the upstream swirling space in a cross sectional surface perpendicular to the center axis.
  • the downstream swirling space has a circular shape in a cross sectional surface perpendicular to the center axis.
  • the fluid swirls in an upstream swirling space and a downstream swirling space with the result that a fluid pressure in the downstream swirling space on the swirling center side can be reduced to a pressure at which the fluid is depressurized and boiled (cavitation is generated).
  • the fluid in the gas-liquid mixing state where the gas-phase fluid and the liquid-phase fluid in the downstream swirling space on the swirling center side are mixed together is allowed to flow into the nozzle, and can be depressurized.
  • the refrigerant in the gas-liquid mixing state does not mean only the refrigerant in a gas-liquid two-phase state, but includes the refrigerant in a state in which air bubbles are mixed in the refrigerant in a subcooled liquid-phase state.
  • a cross-sectional space of an outlet part is formed into an annular shape along an outer peripheral shape of the upstream swirling space, the fluid flowing out of the upstream swirling space can flow from an outer peripheral side of the downstream swirling space in an axial direction.
  • the fluid flowing out of the upstream swirling space can be restrained from flowing toward the swirling center side of the downstream swirling space which has a hollow rotating body shape.
  • the fluid flowing out of the upstream swirling space can merge into a flow of the liquid-phase fluid staying and circulating in the downstream swirling space from the outer peripheral side toward the nozzle.
  • the flow of fluid staying and circulating in the downstream swirling space is not blocked by the fluid flowing from the upstream swirling space into the downstream swirling space, and the ratio of the gas-phase fluid to the fluid in the gas-liquid mixing state flowing into the nozzle can be restrained from being lowered.
  • the boiling of the liquid-phase fluid in the nozzle can be promoted, and a reduction in the nozzle efficiency of the ejector can be limited.
  • an ejector is used for a vapor compression refrigeration cycle device.
  • the ejector includes a body including a refrigerant inlet port, a swirling space in which a refrigerant flowing from the refrigerant inlet port is swirled, a depressurizing space in which the refrigerant flowing out of the swirling space is depressurized, a suction passage that communicates with a downstream side of the depressurizing space in a refrigerant flow and draws a refrigerant from an external, and a pressurizing space in which an ejection refrigerant ejected from the depressurizing space is mixed with a suction refrigerant drawn from the suction passage.
  • the ejector further includes a passage formation member that includes at least a portion disposed inside the depressurizing space, and a portion disposed inside the pressurizing space, and the passage formation member has a conical shape which increases in cross-sectional area in a direction away from the depressurizing space.
  • a refrigerant passage provided between an inner peripheral surface of the body defining the depressurizing space and an outer peripheral surface of the passage formation member is a nozzle passage functioning as a nozzle that depressurizes and ejects the refrigerant flowing out of the swirling space.
  • a refrigerant passage provided between an inner peripheral surface of the body defining the pressurizing space and an outer peripheral surface of the passage formation member is a diffuser passage functioning as a diffuser that mixes and pressurizes the ejection refrigerant and the suction refrigerant.
  • the swirling space includes an upstream swirling space in which the refrigerant flowing from an external is swirled, and a downstream swirling space in which the refrigerant flowing out of the upstream swirling space is introduced into the nozzle passage with swirling.
  • the upstream swirling space and the downstream swirling space have respective rotating body shapes in which center axes are disposed coaxially with each other.
  • the upstream swirling space has an outlet part through which the refrigerant outflow to the downstream swirling space, and the outlet part has an annular shape along an outer peripheral shape of the upstream swirling space in a cross sectional surface perpendicular to the center axis.
  • the downstream swirling space has a circular shape in a cross sectional surface perpendicular to the center axis.
  • the refrigerant in the gas-liquid mixing state where the gas-phase refrigerant and the liquid-phase refrigerant in the downstream swirling space on the swirling center side are mixed together is allowed to flow into the nozzle passage, and can be depressurized. Further, the refrigerant flowing out of the upstream swirling space can merge into the flow of the liquid-phase refrigerant staying and circulating in the downstream swirling space from the outer peripheral side toward the nozzle passage.
  • the flow of refrigerant staying and circulating in the downstream swirling space is not blocked by the refrigerant flowing from the upstream swirling space into the downstream swirling space, and the ratio of the gas-phase refrigerant to the refrigerant in the gas-liquid mixing state flowing into the nozzle passage can be restrained from being lowered.
  • boiling of the liquid-phase refrigerant in the nozzle passage can be promoted, and a reduction in energy conversion efficiency (corresponding to the nozzle efficiency) when the pressure energy of the refrigerant is converted into a velocity energy can be limited in the nozzle passage of the ejector.
  • the passage formation member is not strictly limited to one having only the shape in which the sectional area increases with distance from the depressurizing space. At least a part of the passage formation member may include a shape in which the sectional area expands with distance from the depressurizing space whereby the diffuser passage has a shape expanding outward with distance from the depressurizing space.
  • “formed into a conical shape” is not limited to a meaning that the passage formation member is formed into a complete conical shape, but includes a shape similar to a cone, a shape partially including the conical shape, or a shape combining the conical shape, a cylindrical shape, or a truncated conical shape.
  • a sectional shape in an axial direction is not limited to an isosceles triangle, and may include a shape that has two sides in a state where an apex is interposed between two sides that are convex toward the inner circumferential side, a shape that has two sides in a state where an apex is interposed between two sides that are convex toward the outer peripheral side, a shape in which the sectional shape is formed in a semicircular shape, or the like.
  • the “rotating body shape” means a solid shape formed by rotating a plane figure around one straight line (center axis) extending on the same plane.
  • annular shape along the outer peripheral shape of the upstream swirling space does not mean only a “complete annular shape”, but means a shape that is formed into a “substantially annular shape” even if the outlet part is divided by a connection part of a member forming the outlet part. Therefore, the annular shape may be configured by combination of two semicircular shapes.
  • FIG. 1 is a schematic diagram of an ejector refrigeration cycle according to a first embodiment of the present disclosure.
  • FIG. 2 is a cross-sectional view along an axis direction of an ejector according to the first embodiment.
  • FIG. 3 is a schematic cross-sectional view illustrating a function of each refrigerant passage of the ejector of the first embodiment.
  • FIG. 4 is a cross-sectional view taken along a line IV-IV in FIG. 3 .
  • FIG. 5 is a Mollier diagram illustrating a state of a refrigerant in the ejector refrigeration cycle according to the first embodiment.
  • FIG. 6 is a cross-sectional view along an axial direction of an ejector according to a second embodiment of the present disclosure.
  • FIG. 7 is a schematic cross-sectional view illustrating a function of each refrigerant passage of the ejector of the second embodiment.
  • FIG. 8 is a cross-sectional view taken along a line VIII-VIII of FIG. 6 .
  • FIG. 9 is a schematic view illustrating an ejector refrigeration cycle according to a third embodiment of the present disclosure.
  • FIG. 10 is a cross-sectional view along an axis direction of an ejector according to the third embodiment.
  • FIG. 11 is a schematic cross-sectional view illustrating a flow of a refrigerant within a swirling space of a depressurizing device in results of simulation analysis by the present inventors.
  • an ejector 13 As illustrated in an overall configuration diagram of FIG. 1 , an ejector 13 according to this embodiment is applied to a refrigeration cycle device having an ejector as a refrigerant depressurizing device, that is, an ejector refrigeration cycle 10 . Moreover, the ejector refrigeration cycle 10 is applied to a vehicle air conditioning apparatus, and performs a function of cooling a blast air which is blown into a vehicle interior that is a space to be air-conditioned.
  • an HFC-based refrigerant (more specifically, R134a) is applied as the refrigerant in the ejector refrigeration cycle 10 , and a vapor compression type subcritical refrigeration cycle in which high pressure-side refrigerant pressure does not exceed critical pressure of the refrigerant is configured.
  • an HFO-based refrigerant for example, R1234yf
  • refrigerator oil for lubricating a compressor 11 is mixed in the refrigerant, and a part of the refrigerator oil circulates in the cycle together with the refrigerant.
  • the compressor 11 draws the refrigerant, increases the pressure of the refrigerant until the refrigerant becomes a high-pressure refrigerant, and discharges the pressurized refrigerant.
  • the compressor 11 of this embodiment is an electric compressor that is configured to accommodate a fixed capacity type compression mechanism 11 a and an electric motor 11 b for driving the compression mechanism 11 a in a single housing.
  • the compression mechanism 11 a various compression mechanisms such as a scroll compression mechanism or a vane compression mechanism are capable of being adopted.
  • the electric motor 11 b controls an operation (rotation speed) of the electric motor according to control signals output from a control device to be described below, and any motor of an AC motor and a DC motor may be applied.
  • the compressor 11 may be an engine driven compressor that is driven by a rotation driving force transmitted via a pulley, a belt, or the like from a vehicle travel engine.
  • a variable capacity compressor that can adjust a refrigerant discharge capacity by a change in discharge capacity, or a fixed capacity type compressor that adjusts the refrigerant discharging capacity by changing an operation rate of the compressor through connection/disconnection of an electromagnetic clutch can be applied.
  • a refrigerant inlet side of a condenser 12 a of a radiator 12 is connected to a discharge port side of the compressor 11 .
  • the radiator 12 is a radiation heat exchanger which performs heat exchange between a high pressure refrigerant discharged from the compressor 11 and a vehicle exterior air (outside air) blown by a cooling fan 12 d to radiate the heat of the high pressure refrigerant for cooling.
  • the heat radiator 12 is a so-called subcooling condenser including: the condenser 12 a , a receiver part 12 b , and a subcooling portion 12 c .
  • the condenser 12 a performs heat exchange between the high pressure gas-phase refrigerant discharged from the compressor 11 and the outside air blown from the cooling fan 12 d , and radiates the heat of the high pressure gas-phase refrigerant to condense the refrigerant.
  • the receiver part 12 b separates gas and liquid of the refrigerant flowing out of the condenser 12 a and stores a surplus liquid-phase refrigerant.
  • the subcooling portion 12 c performs heat exchange between the liquid-phase refrigerant flowing out of the receiver part 12 b and the outside air blown from the cooling fan 12 d to subcool the liquid-phase refrigerant.
  • the cooling fan 12 d is an electric blower of which the rotating speed (the amount of blast air) is controlled by a control voltage output from the control device.
  • a refrigerant inlet port 31 a of the ejector 13 is connected to a refrigerant outlet side of the subcooling portion 12 c of the heat radiator 12 .
  • the ejector 13 functions as a refrigerant depressurizing device for depressurizing the high pressure liquid-phase refrigerant (fluid) of the subcooling state, which flows out of the heat radiator 12 , and allowing the refrigerant to flow out to the downstream side.
  • the ejector 13 also functions as a refrigerant circulating device (refrigerant transport device) for drawing (transporting) the refrigerant (fluid) flowing out of an evaporator 14 to be described later by the suction action of the refrigerant (fluid) ejected at high speed to circulate the refrigerant.
  • the ejector 13 according to this embodiment also functions as a gas-liquid separation device for separating the depressurized refrigerant into gas and liquid.
  • FIGS. 2 to 4 A specific configuration of the ejector 13 will be described with reference to FIGS. 2 to 4 .
  • up and down arrows in FIG. 2 indicate, respectively, up and down directions in a state where the ejector refrigeration cycle 10 is mounted on a vehicle air conditioning apparatus.
  • FIGS. 3 and 4 are schematic cross-sectional views illustrating functions and shapes of the respective refrigerant passages of the ejector 13 , and the same parts as those in FIG. 2 are denoted by identical symbols.
  • the ejector 13 includes a body 30 configured by the combination of plural components.
  • the body 30 has a housing body 31 made of prismatic-cylindrical or circular-cylindrical metal or resin, and forming an outer shell of the ejector 13 .
  • a nozzle body 32 , a middle body 33 , and a lower body 34 are fixed to an interior of the housing body 31 .
  • the housing body 31 is formed with a refrigerant inlet port 31 a , a refrigerant suction port 31 b , a liquid-phase refrigerant outlet port 31 c , and a gas-phase refrigerant outlet port 31 d .
  • the refrigerant inlet port 31 a allows the refrigerant flowed out of the heat radiator 12 to flow into the body 30 .
  • the refrigerant suction port 31 b is configured to draw the refrigerant flowing out of the evaporator 14 .
  • the liquid-phase refrigerant outlet port 31 c allows a liquid-phase refrigerant separated by a gas-liquid separation space 30 f formed within the body 30 to flow out to the refrigerant inlet side of the evaporator 14 .
  • the gas-phase refrigerant outlet port 31 d allows the gas-phase refrigerant separated by the gas-liquid separation space 30 f to flow out to the intake side of the compressor 11 .
  • the refrigerant inlet port 31 a is opened in the center of an upper surface of the housing body 31 . Further, a refrigerant inflow passage 31 e for introducing the refrigerant into the interior of the body 30 from the refrigerant inlet port 31 a is formed into a cylindrical shape having a center axis extended in a vertical direction (vertical direction in FIG. 2 ). Further, the refrigerant inflow passage 31 e introduces the refrigerant flowing from the refrigerant inlet port 31 a into a space formed within the nozzle body 32 . In FIGS. 2 and 3 , the center axis of the refrigerant inflow passage 31 e is indicated by a dashed line.
  • the nozzle body 32 is formed of a substantially conical metal member tapered toward a refrigerant flow direction, and a part of a swirling space 30 a for swirling the refrigerant and a depressurizing space 30 b for depressurizing the refrigerant flowing out of the swirling space 30 a are defined in the interior of the nozzle body 32 .
  • the part of the swirling space 30 a and the depressurizing space 30 b are formed into a rotating body shape by combination of a cylindrical shape and a truncated conical shape.
  • the nozzle body 32 is fixed to the interior of the housing body 31 by press fitting so that the center axis of the space defined in the interior of the nozzle body 32 is disposed coaxially with the center axis of the refrigerant inflow passage 31 e.
  • a swirling promotion member 38 that swirls the refrigerant flowing from the refrigerant inlet port 31 a around the center axis of the refrigerant inflow passage 31 e is fixed in the interior of the refrigerant inflow passage 31 e .
  • the swirling promotion member 38 includes an upper plate 38 a and a lower plate 38 b which are each formed into a disc shape, and whose plate surfaces are disposed in parallel to each other, and multiple flow regulating plates 38 c disposed between those plates 38 a and 38 b.
  • the upper plate 38 a forms a fixing portion for fixing the swirling promotion member 38 to the interior of the refrigerant inflow passage 31 e .
  • an outer peripheral side surface of the upper plate 38 a is press-fitted into an inner peripheral wall surface of the refrigerant inflow passage 31 e .
  • a through-hole that penetrates through front and rear sides of the upper plate 38 a is defined in the center of the upper plate 38 a , and the through-hole configures an inlet part 38 d for allowing the refrigerant flowing from the refrigerant inlet port 31 a to flow toward the nozzle body 32 side.
  • an outer diameter of the lower plate 38 b is formed to be smaller than an inner diameter of the refrigerant inflow passage 31 e . Therefore, a gap formed into an annular shape when viewed from the axial direction of the refrigerant inflow passage 31 e is defined between an outer peripheral side of the lower plate 38 b and an inner peripheral wall surface of the refrigerant inflow passage 31 e .
  • the annular gap configures an outlet part 38 e for allowing the refrigerant flowing into the space between the upper plate 38 a and the lower plate 38 b to flow toward the nozzle body 32 side. No through-hole is defined in the lower plate 38 b.
  • the multiple flow regulating plates 38 c are arranged in an annular shape around the center axis of the refrigerant inflow passage 31 e . Further, the plate surfaces of the respective flow regulating plates 38 c are so tilted or curved as to swirl a flow of the refrigerant around the center axis when viewed from the center axis direction.
  • the refrigerant flowing into the refrigerant inflow passage 31 e from the refrigerant inlet port 31 a flows into the space between the upper plate 38 a and the lower plate 38 b through the inlet part 38 d of the upper plate 38 a .
  • the refrigerant flowing into the space between the upper plate 38 a and the lower plate 38 b flows from the center axis radially outward within the space. In this situation, the refrigerant flows along the plate surfaces of the flow regulating plates 38 c whereby the refrigerant swirls around the center axis.
  • the swirling promotion member 38 partitions the swirling space 30 a below (downstream of) the swirling promotion member 38 .
  • the space defined between the upper plate 38 a and the lower plate 38 b in the interior of the swirling promotion member 38 is an example of an upstream swirling space 301 in which the refrigerant flowing from an external swirls.
  • the outlet part 38 e for allowing the refrigerant to flow out of the space (upstream swirling space 301 ) defined between the upper plate 38 a and the lower plate 38 b is formed into the inner peripheral shape of the refrigerant inflow passage 31 e in a cross-sectional surface perpendicular to the axial direction of the upstream swirling space 301 , that is, an annular shape along the outer peripheral shape of the upstream swirling space 301 .
  • swirling space 30 a below (downstream of) the lower plate 38 b is an example of a downstream swirling space 302 for introducing the refrigerant flowing out of the upstream swirling space 301 toward the depressurizing space 30 b side while swirling.
  • the swirling space 30 a (downstream swirling space 302 ) below the lower plate 38 b is formed into a hollow rotating body shape, that is, a circular shape in a cross-sectional surface perpendicular to the axial direction of the refrigerant inflow passage 31 e . Therefore, in the downstream swirling space 302 , a refrigerant pressure on the center axis side is reduced more than the refrigerant pressure on the outer peripheral side due to the action of a centrifugal force generated by swirling the refrigerant.
  • the refrigerant pressure on the center axis side in the downstream swirling space 302 decreases down to a pressure at which the refrigerant is depressurized and boiled (cavitation is generated).
  • the refrigerant pressure on the center axis side within the downstream swirling space 302 as described above can be adjusted by adjustment of the number or the tilt angle of flow regulating plates 38 c , or by adjustment of the layout of the flow regulating plates 38 c (for example, speed increasing cascade arrangement).
  • the depressurizing space 30 b is defined below the swirling space 30 a (specifically, downstream swirling space 302 ) in the space defined in the nozzle body 32 .
  • the depressurizing space 30 b is formed into a rotating body into which the cylindrical space is coupled with a truncated conical space that gradually spreads toward the refrigerant flow direction continuously from a lower side of the cylindrical space.
  • a passage formation member 35 is disposed in the interior of the depressurizing space 30 b .
  • the passage formation member 35 forms a minimum passage area part 30 m smallest in the refrigerant passage area within the depressurizing space 30 b , and changes the passage area of the minimum passage area part 30 m .
  • the passage formation member 35 is formed in an approximately conical shape which gradually spreads toward a downstream side in a refrigerant flow, and a center axis of the passage formation member 35 is disposed coaxially with the center axis of the refrigerant inflow passage 31 e .
  • the passage formation member 35 is formed into a conical shape having a cross-sectional area increased with distance from the depressurizing space 30 b.
  • the refrigerant passage is formed between an inner peripheral surface of a portion of the nozzle body 32 which defines the depressurizing space 30 b and an outer peripheral surface of the upper side of the passage formation member 35 .
  • the refrigerant passage includes a convergent part 131 and a divergent part 132 .
  • the convergent part 131 is formed on the upstream side of the minimum passage area part 30 m in the refrigerant flow, in which the refrigerant passage area extending to the minimum passage area part 30 m gradually decreases.
  • the divergent part 132 is formed on the downstream side of the minimum passage area part 30 m in the refrigerant flow, in which the refrigerant passage area gradually increases.
  • a sectional shape of the refrigerant passage perpendicular to the axis direction is annular (doughnut shape obtained by removing a smaller-diameter circular shape arranged coaxially from the circular shape).
  • a spread angle of the passage formation member 35 of this embodiment is smaller than a spread angle of the circular truncated conical space of the depressurizing space 30 b , the refrigerant passage area of the divergent part 132 gradually enlarges toward the downstream side in the refrigerant flow.
  • the refrigerant passage defined between the inner peripheral surface of the depressurizing space 30 b and the outer peripheral surface of a top side of the passage formation member 35 is a nozzle passage 13 a that functions as a nozzle by the passage shape.
  • the refrigerant is depressurized, and accelerated and ejected in a state where a flow rate of the refrigerant in the gas-liquid mixing state becomes higher than a two-phase sound velocity.
  • the refrigerant flowing into the nozzle passage 13 a swirls in the swirling space 30 a (specifically, downstream swirling space 302 ), the refrigerant flowing through the nozzle passage 13 a , and the ejected refrigerant that is ejected from the nozzle passage 13 a also have a velocity component in a direction of swirling in the same direction as that of the refrigerant swirling in the swirling space 30 a (upstream swirling space 301 and downstream swirling space 302 ).
  • the middle body 33 is formed of a disc-shaped member made of metal which defines a through-hole of the rotating body shape which penetrates through both sides thereof in the center of the middle body 33 .
  • the middle body 33 accommodates a driving device 37 on an outer peripheral side of the through-hole, and the driving device 37 displaces the passage formation member 35 .
  • a center axis of the through-hole is arranged coaxially with the center axes of the refrigerant inflow passage 31 e and the passage formation member 35 .
  • the middle body 33 is fixed to the interior of the housing body 31 and the lower side of the nozzle body 32 by press fitting.
  • An inflow space 30 c is provided between an upper surface of the middle body 33 and an inner wall surface of the housing body 31 facing the middle body 33 , and the inflow space 30 c accumulates the refrigerant flowing from the refrigerant suction port 31 b . Meanwhile, in this embodiment, because a tapered tip of a lower side of the nozzle body 32 is located within the through-hole of the middle body 33 , the inflow space 30 c is formed into an annular shape in cross-section when viewed from the center axis direction of the refrigerant inflow passage 31 e and the passage formation member 35 .
  • a suction refrigerant inflow passage connecting the refrigerant suction port 31 b and the inflow space 30 c extends in a tangential direction of the inner peripheral wall surface of the inflow space 30 c when viewed from the center axis direction of the inflow space 30 c .
  • the refrigerant flowing into the inflow space 30 c from the refrigerant suction port 31 b through the suction refrigerant inflow passage is swirled in the same direction as that of the refrigerant in the swirling space 30 a (upstream swirling space 301 and downstream swirling space 302 ).
  • the through-hole of the middle body 33 has a part in which a refrigerant passage area is gradually reduced toward the refrigerant flow direction so as to match an outer peripheral shape of the tapered tip of the nozzle body 32 in an area where the lower side of the nozzle body 32 is inserted, that is, an area in which the middle body 33 and the nozzle body 32 overlap with each other when viewed in a radial direction perpendicular to the axis line.
  • a suction passage 30 d is defined between an inner peripheral surface of the through-hole and an outer peripheral surface of the lower side of the nozzle body 32 , and the inflow space 30 c communicates with a downstream side of the depressurizing space 30 b in the refrigerant flow through the suction passage 30 d . That is, in this embodiment, a suction passage 13 b that draws the refrigerant from the external is defined by the inflow space 30 c , and the suction passage 30 d .
  • a cross-section perpendicular to the center axis of the suction passage 13 b is also formed into an annular shape, and the drawn refrigerant flows in the suction passage 13 b from the outer peripheral side toward the inner peripheral side of the center axis while swirling.
  • a pressurizing space 30 e formed into a substantially circular truncated conical shape that gradually spreads in the refrigerant flow direction is formed in the through-hole of the middle body 33 on the downstream side of the suction passage 30 d in the refrigerant flow.
  • the pressurizing space 30 e is a space in which the ejected refrigerant ejected from the above-mentioned nozzle passage 13 a is mixed with the suction refrigerant drawn from the suction passage 30 d.
  • the lower side of the above-mentioned passage formation member 35 is located in the interior of the pressurizing space 30 e . Further, a spread angle of the conical-shaped side surface of the passage formation member 35 in the pressurizing space 30 e is smaller than a spread angle of the circular truncated conical space of the pressurizing space 30 e . Therefore, the refrigerant passage area of the refrigerant passage is gradually enlarged toward the downstream side in the refrigerant flow.
  • the refrigerant passage area is enlarged as above.
  • the refrigerant passage which is formed between the inner peripheral surface of the middle body 33 and the outer peripheral surface of the lower side of the passage formation member 35 and configures the pressurizing space 30 e , is defined as a diffuser passage 13 c which functions as a diffuser.
  • the diffuser passage 13 c converts velocity energies of a mixed refrigerant of the ejection refrigerant and the suction refrigerant into a pressure energy. That is, in the diffuser passage 13 c , the ejection refrigerant and the suction refrigerant are mixed together, and pressurized.
  • the cross-sectional shape perpendicular to the center axis of the diffuser passage 13 c is also formed into an annular shape.
  • the refrigerant ejected from the nozzle passage 13 a toward the diffuser passage 13 c side and the refrigerant drawn from the suction passage 13 b have a velocity component in the same swirling direction as that of the refrigerant swirling in the swirling space 30 a (upstream swirling space 301 and downstream swirling space 302 ). Therefore, the refrigerant flowing in the diffuser passage 13 c and the refrigerant flowing out of the diffuser passage 13 c also have a velocity component in the same swirling direction as that of the refrigerant swirling in the swirling space 30 a (upstream swirling space 301 and downstream swirling space 302 ).
  • the driving device 37 that is arranged within the middle body 33 and displaces the passage formation member 35 will be described.
  • the driving device 37 is configured with a circular laminated diaphragm 37 a which is a pressure responsive member. More specifically, as illustrated in FIG. 2 , the diaphragm 37 a is fixed by welding so as to partition a cylindrical space defined on the outer peripheral side of the middle body 33 into two upper and lower spaces.
  • the upper space (the inflow space 30 c side) of the two spaces partitioned by the diaphragm 37 a configures a sealed space 37 b in which a temperature sensitive medium is enclosed.
  • a pressure of the temperature sensitive medium changes according to a temperature of the refrigerant flowing out of the evaporator 14 .
  • a temperature sensitive medium having the same composition as that of the refrigerant circulating through the ejector type refrigeration cycle 10 is sealed in the sealed space 37 b at predetermined density. Accordingly, the temperature sensitive medium of this embodiment is R134a.
  • the lower space of the two spaces partitioned by the diaphragm 37 a configures an introduction space 37 c into which the refrigerant flowing out of the evaporator 14 is introduced through a non-shown communication channel. Therefore, the temperature of the refrigerant flowing out of the evaporator 14 is transmitted to the temperature sensitive medium enclosed in the sealed space 37 b via a cap member 37 d and the diaphragm 37 a that partition the inflow space 30 c and the sealed space 37 b.
  • the suction passage 13 b is arranged on the upper side of the middle body 33 in this embodiment, and the diffuser passage 13 c is arranged on the lower side of the middle body 33 . Therefore, at least a part of the driving device 37 is arranged at a position sandwiched by the suction passage 13 b and the diffuser passage 13 c from the vertical direction when viewed from the radial direction of the axis line.
  • the sealed space 37 b of the driving device 37 is arranged at a position where the suction passage 13 b overlaps with the diffuser passage 13 c and at a position surrounded by the suction passage 13 b and the diffuser passage 13 c when viewed from a center axis direction of the refrigerant inflow passage 31 e and the passage formation member 35 . Accordingly, the temperature of the refrigerant flowing out from the evaporator 14 is transmitted to the sealed space 37 b , and an inner pressure in the sealed space 37 b becomes a pressure corresponding to the temperature of the refrigerant flowing out from the evaporator 14 .
  • the diaphragm 37 a is deformed according to a differential pressure between the internal pressure of the sealed space 37 b and the pressure of the refrigerant which has flowed into the introduction space 37 c from the evaporator 14 .
  • the diaphragm 37 a is made of a material rich in elasticity, excellent in heat conduction, and tough.
  • the diaphragm 37 a is formed of a metal laminate made of stainless steel (SUS304).
  • An upper end side of a cylindrical actuating bar 37 e is joined to a center part of the diaphragm 37 a by welding, and a lower end side of the actuating bar 37 e is fixed to an outer peripheral side of the lowermost side (bottom side) of the passage formation member 35 .
  • the diaphragm 37 a and the passage formation member 35 are coupled with each other, and the passage formation member 35 is displaced in accordance with a displacement of the diaphragm 37 a to regulate the refrigerant passage area of the nozzle passage 13 a (passage cross-sectional area in the minimum passage area part 30 m ).
  • the diaphragm 37 a displaces the passage formation member 35 in a direction of enlarging the passage cross-sectional area in the minimum passage area part 30 m (downward in the vertical direction).
  • the diaphragm 37 a displaces the passage formation member 35 in a direction of reducing the passage cross-sectional area of the minimum passage area part 30 m (toward the upper side in the vertical direction).
  • the diaphragm 37 a displaces the passage formation member 35 vertically according to the superheat of the refrigerant flowing out of the evaporator 14 as described above.
  • the passage cross-sectional area of the minimum passage area part 30 m is adjusted so that the degree of superheat of the refrigerant flowing out of the evaporator 14 comes closer to a predetermined value.
  • a gap between the actuating bar 37 e and the middle body 33 is sealed by a seal member such as an O-ring not shown, and the refrigerant is not leaked through the gap even if the actuating bar 37 e is displaced.
  • the bottom of the passage formation member 35 is subjected to a load of a coil spring 40 fixed to the lower body 34 .
  • the coil spring 40 exerts the load urging the passage formation member 35 so as to reduce the passage cross-sectional area in the minimum passage area part 30 m (upper side in FIG. 2 ). With the regulation of this load, a valve opening pressure of the passage formation member 35 can be changed to change a target degree of superheat.
  • the multiple (specifically, two as illustrated in FIGS. 2 and 3 ) cylindrical spaces are provided in the part of the middle body 33 on the radially outer side, and the respective circular laminated diaphragms 37 a are fixed in those spaces to configure two driving devices 37 .
  • the number of driving devices 37 is not limited to this number.
  • the driving devices 37 are provided at plural locations, it is desirable that the driving devices 37 are arranged at regular angular intervals with respect to the respective center axes.
  • a diaphragm formed of the annular thin plate may be fixed in a space having an annular shape when viewed from the center axis direction, and the diaphragm and the passage formation member 35 may be coupled with each other by multiple actuating bars.
  • the lower body 34 is formed of a circular-cylindrical metal member, and fixed in the housing body 31 by screwing so as to close a bottom of the housing body 31 .
  • the gas-liquid separation space 30 f that separates gas and liquid of the refrigerant that has flowed out of the above-mentioned diffuser passage 13 c from each other is defined between the upper side of the lower body 34 and the middle body 33 .
  • the gas-liquid separation space 30 f is defined as a space of a substantially cylindrical rotating body shape, and the center axis of the gas-liquid separation space 30 f is also arranged coaxially with the center axes of the refrigerant inflow passage 31 e and the passage formation member 35 .
  • the refrigerant which flows out from the diffuser passage 13 c and flows into the gas-liquid separation space 30 f , has the velocity component of the refrigerant swirling in the same direction as the swirl direction of the refrigerant swirling in the swirling space 30 a (upstream swirling space 301 and downstream swirling space 302 ). Accordingly, gas and liquid of the refrigerant in the gas-liquid separation space 30 f are separated by action of a centrifugal force.
  • a hollow cylindrical pipe 34 a that is arranged coaxially with the gas-liquid separation space 30 f and extends upward is disposed in the center part of the lower body 34 .
  • the liquid-phase refrigerant separated in the gas-liquid separation space 30 f is accumulated on a radially outer side of the pipe 34 a .
  • a gas-phase refrigerant outflow passage 34 b is formed inside the pipe 34 a and guides the gas-phase refrigerant separated in the gas-liquid separation space 30 f to the gas-phase refrigerant outlet port 31 d of the housing body 31 .
  • the above-mentioned coil spring 40 is fixed to an upper end of the pipe 34 a .
  • the coil spring 40 also functions as a vibration absorbing member that attenuates the vibration of the passage formation member 35 , which is caused by a pressure pulsation generated when the refrigerant is depressurized.
  • An oil return hole 34 c that returns a refrigerator oil in the liquid-phase refrigerant into the compressor 11 through the gas-phase refrigerant outflow passage 34 b is formed on a base part (lowermost part) of the pipe 34 a.
  • the liquid-phase refrigerant outlet port 31 c of the ejector 13 is connected with an inlet side of the evaporator 14 as illustrated in FIG. 1 .
  • the evaporator 14 is a heat-absorbing heat exchanger that evaporates a low-pressure refrigerant depressurized by the ejector 13 and performs a heat absorbing effect by exchanging heat between the low-pressure refrigerant and blast air that is blown into the vehicle interior from a blower fan 14 a.
  • the blower fan 14 a is an electric blower of which the rotation speed (the amount of blast air) is controlled by a control voltage output from the control device.
  • the refrigerant suction port 31 b of the ejector 13 is connected to an outlet side of the evaporator 14 . Further, the gas-phase refrigerant outlet port 31 d of the ejector 13 is connected with the intake side of the compressor 11 .
  • control device includes a well-known microcomputer including a CPU, a ROM and a RAM, and peripheral circuits of the microcomputer.
  • the control device controls the operations of the above-mentioned various electric actuators 11 b , 12 d , and 14 a and the like by performing various calculations and processing on the basis of a control program stored in the ROM.
  • an air conditioning control sensor group such as an inside air temperature sensor for detecting a vehicle interior temperature, an outside air temperature sensor for detecting the temperature of outside air, an insolation sensor for detecting the amount of insolation in the vehicle interior, an evaporator-temperature sensor for detecting the blow-out air temperature from the evaporator 14 (the temperature of the evaporator), an outlet-side temperature sensor for detecting the temperature of a refrigerant on the outlet side of the heat radiator 12 , and an outlet-side pressure sensor for detecting the pressure of a refrigerant on the outlet side of the heat radiator 12 , is connected to the control device. Accordingly, detection values of the sensor group are input to the control device.
  • an operation panel (not shown), which is disposed near a dashboard panel positioned at the front part in the vehicle interior, is connected to the input side of the control device, and operation signals output from various operation switches mounted on the operation panel are input to the control device.
  • An air conditioning operation switch that is used to perform air conditioning in the vehicle interior, a vehicle interior temperature setting switch that is used to set the temperature of the vehicle interior, and the like are provided as the various operation switches that are mounted on the operation panel.
  • control device of this embodiment is integrated with a control unit for controlling the operations of various control target devices connected to the output side of the control device, but a structure (hardware and software), which controls the operations of the respective control target devices, of the control device forms the control unit of the respective control target devices.
  • a structure (hardware and software), which controls the operation of the electric motor 11 b of the compressor 11 forms a discharge capability control unit in this embodiment.
  • a vertical axis of the Mollier diagram indicates pressures corresponding to P 0 , P 1 , and P 2 of FIG. 3 .
  • the control device operates the electric motor 11 b of the compressor 11 , the cooling fan 12 d , the blower fan 14 a , or the like. Accordingly, the compressor 11 draws and compresses a refrigerant and discharges the refrigerant.
  • the gas-phase refrigerant (point a 5 in FIG. 5 ), which is discharged from the compressor 11 and has a high temperature and a high pressure, flows into the condenser 12 a of the heat radiator 12 and is condensed by exchanging heat between the blast air (outside air), which is blown from the cooling fan 12 d , and itself and by radiating heat. Gas and liquid of the refrigerant radiated by the condenser 12 a are separated by the receiver part 12 b .
  • the subcooled liquid-phase refrigerant that has flowed out of the subcooling portion 12 c of the heat radiator 12 is isentropically depressurized by the nozzle passage 13 a , and ejected (from point b 5 to point c 5 in FIG. 5 ).
  • the nozzle passage 13 a is formed between the inner peripheral surface of the depressurizing space 30 b of the ejector 13 and the outer peripheral surface of the passage formation member 35 .
  • the refrigerant passage area in the minimum passage area part 30 m of the depressurizing space 30 b is regulated so that the degree of superheat of the refrigerant on the outlet side of the evaporator 14 comes close to a predetermined given value.
  • the refrigerant that has flowed out of the evaporator 14 is drawn through the refrigerant suction port 31 b and the suction passage 13 b (in more detail, the inflow space 30 c and the suction passage 30 d ) due to the suction action of the ejection refrigerant which has been ejected from the nozzle passage 13 a .
  • the ejection refrigerant ejected from the nozzle passage 13 a and the suction refrigerant drawn through the suction passage 13 b and the like flow into the diffuser passage 13 c (from point c 5 to point d 5 , and from point h 5 to point d 5 in FIG. 5 ).
  • the velocity energy of the refrigerant is converted into the pressure energy due to the enlarged refrigerant passage area.
  • the mixed refrigerant is pressurized while the ejection refrigerant and the suction refrigerant are mixed together (from point d 5 to point e 5 in FIG. 5 ).
  • the refrigerant that has flowed out of the diffuser passage 13 c is separated into gas and liquid in the gas-liquid separation space 30 f (from point e 5 to point f 5 , and from point e 5 to point g 5 in FIG. 5 ).
  • the liquid-phase refrigerant that has been separated in the gas-liquid separation space 30 f flows out of the liquid-phase refrigerant outlet port 31 c , and flows into the evaporator 14 .
  • the refrigerant which has flowed into the evaporator 14 absorbs heat from blown air blown by the blower fan 14 a , is evaporated, and cools the blast air (point g 5 to point h 5 in FIG. 5 ).
  • the gas-phase refrigerant that has been separated in the gas-liquid separation space 30 f flows out of the gas-phase refrigerant outlet port 31 d , and is drawn into the compressor 11 and compressed again (point f 5 to point a 5 in FIG. 5 ).
  • the ejector refrigeration cycle 10 operates as described above, and can cool the blast air to be blown into the vehicle interior. Further, in the ejector refrigeration cycle 10 , since the refrigerant pressurized by the diffuser passage 13 c is drawn into the compressor 11 , the drive power of the compressor 11 can be reduced to improve the cycle of performance (COP).
  • COP cycle of performance
  • the fluid swirls in the upstream swirling space 301 and the downstream swirling space 302 with the result that a fluid pressure in the downstream swirling space 302 on the swirling center side can be reduced to a pressure at which the refrigerant is depressurized and boiled (cavitation is generated). Further, the refrigerant in the gas-liquid mixing state where the gas-phase refrigerant and the liquid-phase refrigerant in the downstream swirling space 302 on the swirling center side are mixed together is allowed to flow into the nozzle passage 13 a , and can be depressurized.
  • a state of the refrigerant in the vicinity of the minimum passage area part 30 m approaches the gas-liquid mixing state in which the gas-phase refrigerant and the liquid-phase refrigerant are homogeneously mixed together, and blocking (choking) is generated in a flow of the refrigerant of the gas-liquid mixing state.
  • the flow rate of the refrigerant can be accelerated to the sound velocity or higher.
  • the refrigerant in the gas-liquid mixing state which is a supersonic state flows into the divergent portion 132 so as to be further accelerated and ejected. Therefore, the effective improvement in the energy conversion efficiency in converting the pressure energy of the refrigerant into the velocity energy in the nozzle passage 13 a can be expected.
  • the sectional shape of the outlet part 38 e for allowing the refrigerant to flow out of the upstream swirling space 301 is formed into an annular shape along the outer peripheral shape of the upstream swirling space 301 , the refrigerant flowing out of the upstream swirling space 301 can flow in the axial direction from the outer peripheral side of the downstream swirling space 302 as indicated by solid arrows in FIG. 3 .
  • the refrigerant flowing out of the upstream swirling space 301 can be restrained from flowing toward the swirling center side of the downstream swirling space 302 . Further, the refrigerant flowing out of the upstream swirling space 301 can merge into the flow from the outer peripheral side of the downstream swirling space 302 toward the nozzle passage 13 a side, of the flow (flow indicated by dashed arrows in FIG. 3 ) of the liquid-phase refrigerant staying while circulating in the downstream swirling space 302 .
  • the flow of refrigerant staying while circulating in the downstream swirling space 302 is not blocked by the refrigerant flowing from the upstream swirling space 301 into the downstream swirling space 302 , and the ratio of the gas-phase refrigerant to the refrigerant in the gas-liquid mixing state flowing into the nozzle passage 13 a can be restrained from being lowered.
  • the boiling of the liquid-phase refrigerant in the nozzle passage 13 a is promoted, and the energy conversion efficiency in the nozzle passage 13 a can be restrained from being lowered.
  • the upstream swirling space 301 is defined in a space between the upper plate 38 a and the lower plate 38 b , and the swirling promotion member 38 that swirls the refrigerant within the upstream swirling space 301 around the center axis by allowing the refrigerant on the center side of the upstream swirling space 301 to flow toward the outer peripheral side along the plate surface of the flow regulating plates 38 c is provided.
  • the shape of the outlet part 38 e for allowing the refrigerant to flow out of the upstream swirling space 301 can be easily formed into an annular shape along the outer peripheral shape of the upstream swirling space 301 . Further, since there is no need to provide the space for generating the swirling flow of the refrigerant outside the upstream swirling space 301 , the body size can be restrained from being upsized as the overall ejector 13 .
  • the ejector 13 of this embodiment employs the passage formation member 35 having a conical shape of which a cross-sectional area increases with distance from the depressurizing space 30 b .
  • the cross-sectional shape of the diffuser passage 13 c is formed in an annular shape. Therefore, the diffuser passage 13 c can have a shape to spread along the outer periphery of the passage formation member 35 in a direction away from the depressurizing space 30 b.
  • the dimension of the diffuser passage 13 c in an axial direction (axial direction of the passage formation member 35 ) can be restrained from increasing.
  • the upsizing of the body of the overall ejector 13 can be limited.
  • the gas-liquid separation space 30 f that separates gas and liquid of the refrigerant that has flowed out of the diffuser passage 13 c is formed in the body 30 of the ejector 13 according to this embodiment.
  • the capacity of the gas-liquid separation space 30 f can be effectively reduced as compared with a case in which a gas-liquid separation device is provided in addition to the ejector 13 .
  • the capacity of the gas-liquid separation space 30 f can be effectively reduced as compared with the case in which the gas-liquid separation device is provided apart from the ejector 13 .
  • FIGS. 6 to 8 correspond to FIGS. 2 to 4 in the first embodiment, respectively, and the same or equivalent parts to those in the first embodiment are denoted by identical symbols.
  • a swirling promotion member 39 includes a plate 39 a formed into a disc shape, multiple flow regulating plates 39 b projected downward from an outer peripheral part of the plate 39 a , and a cylindrical protruding portion 39 c projected from a center part of the plate 39 a toward the same direction (downward) as that of the flow regulating plates 39 b .
  • the amount of projection from the plate 39 a of the protruding portion 39 c is equal to or larger than the amount of projection of the flow regulating plates 39 b.
  • An outer diameter of the refrigerant inflow passage 31 e is formed to be larger than an outer diameter of a space defined in the interior of the nozzle body 32 , and an outer diameter of the plate 39 a is formed to be smaller than an outer diameter of the refrigerant inflow passage 31 e . Therefore, a gap formed into an annular shape when viewed from the axial direction of the refrigerant inflow passage 31 e is defined between an outer peripheral side of the plate 39 a and an inner peripheral wall surface of the refrigerant inflow passage 31 e . The annular gap configures an inlet part 39 d for allowing the refrigerant flowing from the refrigerant inlet port 31 a toward the nozzle body 32 side.
  • the multiple flow regulating plates 39 b are arranged in an annular shape around the center axis of the refrigerant inflow passage 31 e . Further, the plate surfaces of the respective flow regulating plates 39 b are so tilted or curved as to swirl a flow of the refrigerant around the center axis when viewed from the center axis direction. Those flow regulating plates 39 b are disposed in an area extending from an outer periphery of the plate 39 a to an outer periphery of a space defined in the interior of the nozzle body 32 when viewed from the center axis direction.
  • the center axis of the protruding portion 39 c is disposed coaxially with the center axis of the refrigerant inflow passage 31 e , and an outer diameter of the protruding portion 39 c is formed to be smaller than an outer diameter of the space defined in the interior of the nozzle body 32 . Therefore, a hollow cylindrical gap space formed in an annular shape in a cross-section perpendicular to the center axis direction is defined between the inner peripheral side of the multiple flow regulating plates 39 b disposed annularly and the outer peripheral side of the protruding portion 39 c.
  • the refrigerant flowing into the refrigerant inflow passage 31 e from the refrigerant inlet port 31 a flows into the outer peripheral side of the multiple flow regulating plates 39 b disposed annularly through the inlet part 39 d on the outer peripheral side of the plate 39 a . Further, the refrigerant flowing into the outer peripheral side of the multiple flow regulating plates 39 b flows toward the inner peripheral side of the multiple flow regulating plates 39 b . In this situation, the refrigerant flows along the plate surfaces of the multiple flow regulating plates 39 b whereby the refrigerant swirls around the center axis.
  • the refrigerant flowing into the inner peripheral side of the multiple flow regulating plates 39 b flows into the hollow cylindrical gap space defined between the inner peripheral side of the multiple flow regulating plates 39 b and the outer peripheral side of the protruding portion 39 c .
  • the refrigerant flowing into the hollow cylindrical gap space flows into the space below (downstream side) of the swirling promotion member 39 from a lowermost side of the hollow cylindrical gap space while swirling around the center axis. Further, the refrigerant flowing into the space below the swirling promotion member 39 is introduced into the nozzle passage 13 a side to be described later while swirling around the center axis.
  • the hollow cylindrical gap space defined between the inner peripheral side of the flow regulating plates 39 b and the outer peripheral side of the protruding portion 39 c is an example of the upstream swirling space 301 in which the refrigerant flowing from the external is swirled.
  • the outlet part 39 e disposed on a lowermost part (downstream side) of the hollow cylindrical gap space (upstream swirling space 301 ) for allowing the refrigerant to flow out of the upstream swirling space 301 is formed into an annular shape similar to the cross-sectional shape of the upstream swirling space 301 in a cross sectional surface perpendicular to the axial direction, that is, an annular shape along the outer peripheral shape of the upstream swirling space 301 .
  • the space below (downstream of) the swirling promotion member 39 is an example of a downstream swirling space 302 for introducing the refrigerant flowing out of the upstream swirling space 301 toward the depressurizing space 30 b side while swirling.
  • the other configuration and operation of the ejector 13 and the ejector refrigeration cycle 10 are similar to those of the first embodiment.
  • the refrigerant (flow indicated by thick solid arrows in FIG. 7 ) flowing out of the upstream swirling space 301 can merge into the flow from the outer peripheral side of the downstream swirling space 302 toward the nozzle passage 13 a side, of the flow (flow indicated by dashed arrows in FIG. 7 ) of the liquid-phase refrigerant staying and circulating in the downstream swirling space 302 .
  • a reduction in the energy conversion efficiency in the nozzle passage 13 a can be limited.
  • the shape of the outlet part 38 e for allowing the refrigerant to flow out of the upstream swirling space 301 can be easily formed into an annular shape along the outer peripheral shape of the upstream swirling space 301 .
  • the swirling flow of the refrigerant is generated on the outer peripheral side of the upstream swirling space 301 , and the refrigerant having the velocity component in a direction of swirling around the center axis flows into the upstream swirling space 301 . Therefore, when a configuration in which the swirling flow of the refrigerant is generated in the interior of the upstream swirling space 301 is disposed, the degree of freedom of design of the configuration in which the swirling flow of the refrigerant is generated can be improved.
  • the ejector 13 according to the first embodiment is replaced with an ejector 53 and a gas-liquid separator 60 .
  • the ejector 53 does not have a function of the gas-liquid separator, but as in the ejector 13 of the first embodiment, performs a function of a refrigerant depressurizing device and also performs a function of a refrigerant circulation device (refrigerant transport device).
  • a specific configuration of the ejector 53 will be described with reference to FIG. 10 .
  • the ejector 53 has a nozzle 531 and a body 532 as illustrated in FIG. 10 .
  • the nozzle 531 is made of metal (for example, stainless alloy) shaped into substantially a hollow cylinder gradually tapered toward a flowing direction of the refrigerant, and the refrigerant flowing into the nozzle 531 is isentropically depressurized, and ejected from a refrigerant ejection port 531 a defined on the most downstream side in the refrigerant flow.
  • the interior of the nozzle 531 is formed with a swirling space 531 c in which the refrigerant flowing from a refrigerant inlet port 531 b swirls, and a refrigerant passage in which the refrigerant flowing out of the swirling space 531 c is depressurized.
  • the swirling space 531 c is formed in the interior of a cylindrical part 531 g disposed on the upstream side of the nozzle 531 in the refrigerant flow. Therefore, the cylindrical part 531 g may be used as an example of a swirling space formation member having the swirling space 531 c , and in this embodiment, the swirling space formation member and the nozzle are integrated with each other.
  • a cylindrical member 531 h formed into a cylindrical shape smaller than an inner diameter of the cylindrical part 531 g is disposed on the upstream side in the refrigerant flow in the interior of the cylindrical part 531 g .
  • the axial length of the cylindrical member 531 h is formed to be shorter than an axial length of the cylindrical part 531 g , and disposed coaxially with a center axis of the cylindrical part 531 g.
  • a hollow cylindrical space formed into an annular shape in a cross-section perpendicular to the center axis direction is defined between the inner peripheral side of the cylindrical part 531 g and the outer peripheral side of the cylindrical member 531 h .
  • a cylindrical space formed into a circular shape in a cross-section perpendicular to the center axis direction is defined on the inner peripheral side of the cylindrical part 531 g.
  • a refrigerant inflow passage that connects the refrigerant inlet port 531 b and the swirling space 531 c is opened in the hollow cylindrical space, and extends in a tangential direction of an inner wall surface of the swirling space 531 c when viewed from a center axis direction of the swirling space 531 c.
  • the refrigerant flowing into the hollow cylindrical space from the refrigerant inlet port 531 b flows along an inner peripheral wall surface of the cylindrical part 531 g , and swirls about a center axis of the cylindrical part 531 g . Further, the refrigerant flowing out of the hollow cylindrical space flows into the cylindrical space while swirling around the center axis.
  • the hollow cylindrical space within the cylindrical part 531 g is an example of an upstream swirling space 311 in which the refrigerant flowing out of the external is swirled
  • the cylindrical space within the cylindrical part 531 g is an example of a downstream swirling space 312 that introduces the refrigerant flowing out of the upstream swirling space 311 into a minimum passage area part 531 d of the nozzle 531 while swirling.
  • An outlet part 311 a disposed on the most downstream side of the hollow cylindrical space (upstream swirling space 311 ) for allowing the refrigerant to flow out of the upstream swirling space 311 is formed into an annular shape similar to the cross-sectional shape of the upstream swirling space 311 in a cross sectional surface perpendicular to the axial direction, that is, an annular shape along the outer peripheral shape of the upstream swirling space 311 .
  • downstream swirling space 312 is formed into the hollow rotating body shape, a refrigerant pressure on the center axis side is reduced more than the refrigerant pressure on the outer peripheral side due to the action of a centrifugal force generated by swirling the refrigerant in the downstream swirling space 312 . Accordingly, in this embodiment, in a normal operation of the ejector refrigeration cycle 10 , the refrigerant pressure on the center axis side in the downstream swirling space 312 is reduced to a pressure at which the refrigerant is depressurized and boiled (cavitation is generated).
  • the adjustment of the refrigerant pressure on the center axis side in the downstream swirling space 312 can be realized by adjusting the swirling flow rate of the refrigerant swirling in the downstream swirling space 312 .
  • the swirling flow rate can be adjusted by, for example, adjusting an area ratio of the passage sectional area of the refrigerant inflow passage to the sectional area of the downstream swirling space 312 perpendicular to the axial direction.
  • the swirling flow rate in this embodiment means the flow rate of the refrigerant in the swirling direction in the vicinity of the outermost peripheral part of the swirling space 531 c.
  • the refrigerant passage defined in the interior of the nozzle 531 is formed with the minimum passage area part 531 d having a refrigerant passage area most reduced, a tapered part 531 e having a refrigerant passage area gradually reduced toward the minimum passage area part 531 d from the swirling space 531 c , and a divergent part 531 f having a refrigerant passage area gradually enlarged from the minimum passage area part 531 d toward the refrigerant ejection port 531 a.
  • the body 532 is made of metal (for example, aluminum) or resin formed into substantially a hollow cylindrical shape, functions as a fixing member for internally supporting and fixing the nozzle 531 , and forms an outer shell of the ejector 53 . More specifically, the nozzle 531 is fixed by press fitting so as to be housed in the interior of the body 532 on one end side in the longitudinal direction of the body 532 .
  • a refrigerant suction port 532 a is defined in a portion corresponding to an outer peripheral side of the nozzle 531 on an outer peripheral side surface of the body 532 .
  • the refrigerant suction port 532 a is a through-hole that penetrates through a portion corresponding to an outer peripheral side of the nozzle 531 on the outer peripheral side surface of the body 532 , and disposed to communicate with the refrigerant ejection port 531 a of the nozzle 531 .
  • the refrigerant suction port 532 a draws the refrigerant flowing out of an evaporator 14 into the interior of the ejector 53 due to the suction action of the ejection refrigerant ejected from the refrigerant ejection port 531 a of the nozzle 531 .
  • the refrigerant suction port 532 a may be used as an example of the fluid suction port for drawing the fluid due to the suction action of the ejected fluid at a high speed which is ejected from the nozzle 531 .
  • the body 532 internally includes a diffuser portion 532 b that mixes the ejection refrigerant ejected from the refrigerant ejection port 531 a with the suction refrigerant drawn from the refrigerant suction port 532 a to increase the pressure, and a suction passage 532 c that introduces the suction refrigerant drawn from the refrigerant suction port 532 a into the diffuser portion 532 b .
  • the diffuser portion 532 b may be used as an example of a pressure increase part for mixing and pressurizing the ejection fluid ejected from the nozzle 531 with the suction fluid drawn from the fluid suction port.
  • the suction passage 532 c is formed by a space between an outer peripheral side around a tip of a tapered shape of the nozzle 531 and an inner peripheral side of the body 532 .
  • a refrigerant passage area of the suction passage 532 c is gradually reduced toward the refrigerant flow direction.
  • the diffuser portion 532 b is disposed to be continuous to an outlet side of the suction passage 532 c , and formed so that a refrigerant passage area gradually increases.
  • This configuration performs a function of converting a velocity energy of a mixed refrigerant of the ejection refrigerant and the suction refrigerant into a pressure energy, that is, functions as a pressure increase part that decelerates a flow rate of the mixed refrigerant, and pressurizes the mixed refrigerant.
  • a wall surface shape of the inner peripheral wall surface of the body 532 forming the diffuser portion 532 b according to this embodiment is defined by the combination of multiple curves as illustrated in a cross-section along the axial direction in FIG. 2 .
  • a spread degree of the refrigerant passage cross-sectional area of the diffuser portion 532 b gradually increases toward the refrigerant flow direction, and thereafter again decreases, as a result of which the refrigerant can be isentropically pressurized.
  • a refrigerant outlet side of the diffuser portion 532 b of the ejector 53 is connected with a refrigerant inlet port of the gas-liquid separator 60 .
  • the gas-liquid separator 60 is a gas-liquid separation device that separates gas and liquid of the refrigerant flowing into the interior of the gas-liquid separator 60 from each other.
  • a liquid-phase refrigerant outlet port of the gas-liquid separator 60 is connected with the refrigerant inlet side of the evaporator 14 .
  • the gas-phase refrigerant outlet port of the gas-liquid separator 60 is connected with an inlet side of the compressor 11 .
  • Other structures and operations are the same as those of the first embodiment.
  • the refrigerant flowing out of the upstream swirling space 311 (a flow indicated by dashed arrows in FIG. 10 ) can merge into the flow from the outer peripheral side of the downstream swirling space 312 toward the minimum passage area part 531 d side of the nozzle 531 , of the flow (flow indicated by dashed arrows in FIG. 10 ) of the liquid-phase refrigerant staying and circulating in the downstream swirling space 312 .
  • a reduction in the nozzle efficiency of the nozzle 531 can be limited.
  • the refrigerant inflow passage 31 e is defined to extend in the tangential direction of the inner wall surface of the swirling space 30 a , and the same cylindrical member as that in the third embodiment is disposed in the interior of the swirling space 30 a .
  • the hollow cylindrical space defined in the area where the swirling space 30 a overlaps with the cylindrical member may be defined as the upstream swirling space 301
  • the cylindrical space defined in the area where the swirling space 30 a does not overlap with the cylindrical member may be defined as the downstream swirling space 302 .
  • the swirling promotion members 38 and 39 according to the first and second embodiments are disposed in the interior of the cylindrical part 531 g .
  • the upstream swirling space 311 and the downstream swirling space 312 may be defined.
  • the driving device 37 that displaces the passage formation member 35 includes the sealed space 37 b in which the temperature sensitive medium having the pressure changed according to a change in the temperature is sealed, and the diaphragm 37 a that is displaced according to the pressure of the temperature sensitive medium within the sealed space 37 b .
  • the driving device is not limited to this configuration.
  • thermo wax that changes a volume with temperature as a temperature sensitive medium may be applied, or the driving device formed of a shape memory alloy elastic member as a driving device may be applied.
  • the driving device in which the passage formation member 35 is displaced by an electric motor may be applied as the driving device as in the second embodiment.
  • the axial direction of the nozzle 531 may be disposed in parallel to a vertical direction as in the first and second embodiments, or may be disposed in parallel to another direction (for example, a horizontal direction). This is because the refrigerant swirling within the swirling space 531 c is unlikely to be affected by a gravity force because the swirling speed is relatively high.
  • a depressurizing device for example, side fixed aperture formed of an orifice or a capillary tube for depressurizing the refrigerant may be arranged on those refrigerant outlet ports.
  • the ejector refrigeration cycle 10 including the ejector 13 of the present disclosure is applied to a vehicle air conditioning apparatus
  • the application of the ejector refrigeration cycle 10 having the ejector 13 of the present disclosure is not limited to this configuration.
  • the ejector refrigeration cycle 10 may be applied to, for example, a stationary air conditioning apparatus, cold storage warehouse, a cooling heating device for a vending machine, etc.
  • the present disclosure has been made based on the following analytical findings.
  • the present inventors have confirmed a flow of the refrigerant within the swirling space when the refrigerant pressure on the swirling center side is reduced down to a pressure at which the refrigerant is depressurized and boiled by swirling the refrigerant for refrigeration cycle in the swirling space of the depressurizing device by simulation analysis.
  • FIG. 11 is a cross-sectional view along an axial direction of a swirling space 70 d showing a result of the simulation analysis, in which an area in which the liquid-phase refrigerant is present is indicated by dot hatching, and flow lines of the refrigerant in that area is indicated by respective arrows.
  • the flow lines indicated by the respective arrows are flow lines illustratable in a cross-section in the axial direction in FIG. 11 , that is, flow lines that can be drawn by velocity components from which a velocity component in the swirling direction is removed.
  • the swirling space 70 d is defined within a main body 70 a of a depressurizing device 70 , and formed into a hollow rotating body shape (in more detail, a shape in which a cylindrical space is coupled coaxially with a conical space).
  • gas column A liquid-phase refrigerant around the gas-phase refrigerant (hereinafter referred to as “gas column”) unevenly distributed in the columnar shape flows from a minimum passage area part 70 b side that is one end side along the gas column in the axial direction (lower side in FIG. 11 ) toward the other end side in the axial direction (upper side in FIG. 11 ) as indicated by the flow lines of dashed arrows.
  • the refrigerant that flows along the gas column and reaches the other end side in the axial direction flows on an outer peripheral side of the swirling space 70 d , and flows toward the minimum passage area part 70 b side from the outer peripheral side.
  • the refrigerant that reaches the minimum passage area part 70 b side again flows from the minimum passage area part 70 b side toward the other end side in the axial direction along the gas column.
  • the liquid-phase refrigerant around the gas column stays while circulating around the gas column as indicated by dashed arrows in FIG. 11 .
  • the liquid-phase refrigerant around the gas column stays while circulating, and the liquid-phase refrigerant flows along the gas column from the minimum passage area part 70 b side toward the other end side in the axial direction. Therefore, it is understood that an angular momentum of the swirling flow of the refrigerant in the vicinity of the minimum passage area part 70 b is transmitted to the refrigerant in an overall area on the swirling center side in the axial direction. Further, it is understood that the depressurization and boiling of the refrigerant in the overall area on the swirling center side in the axial direction are promoted by the transmission of the angular momentum, and the gas column is formed over the overall area within the swirling space 70 d in the axial direction.
  • the refrigerant flowing from a refrigerant inlet port 70 c connected to a side surface of the main body 70 a into the swirling space 70 d flows toward the minimum passage area part 70 b side along the outer peripheral side of the refrigerant staying while circulating around the gas column as shown by flow lines indicated by thick solid arrows in FIG. 11 .
  • the refrigerant flowing into the swirling space 70 d is a high pressure refrigerant flowing out of the radiator, even if the refrigerant flows in the tangential direction of the swirling space 70 d circular in the cross-section, the refrigerant flowing into the swirling space 70 d is liable to flow toward the low pressure side (that is, swirling center side) under an operation condition where a pressure of the high pressure refrigerant is relatively high as in a high load operation of the refrigeration cycle device.
  • the refrigerant in the gas-liquid mixing state does not mean only the refrigerant in a gas-liquid two-phase state, but includes the refrigerant in a state where air bubbles are mixed in the refrigerant in a subcooled liquid-phase state.
  • the refrigerant flowing from the refrigerant inlet port 70 c into the swirling space 70 d may merge into a flow from the outer peripheral side toward the minimum passage area part 70 b side, of the refrigerant flow of the liquid-phase refrigerant staying and circulating around the gas column.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Thermal Sciences (AREA)
  • Jet Pumps And Other Pumps (AREA)
US14/890,170 2013-05-15 2014-05-14 Ejector Abandoned US20160090995A1 (en)

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JP2013103141A JP2014224626A (ja) 2013-05-15 2013-05-15 エジェクタ
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150285271A1 (en) * 2014-04-04 2015-10-08 Caltec Limited Jet pump
US20210348810A1 (en) * 2020-05-06 2021-11-11 Carrier Corporation Ejector refrigeration circuit
US20220290694A1 (en) * 2019-08-19 2022-09-15 Q.E.D. Environmental Systems, Inc. Pneumatic fluid pump with dual rotational swirling cleaning action
US20220307733A1 (en) * 2020-07-10 2022-09-29 Energy Recovery, Inc. Low energy consumption refrigeration system with a rotary pressure exchanger replacing the bulk flow compressor and the high pressure expansion system
US11982481B2 (en) 2020-07-10 2024-05-14 Energy Recovery, Inc. Refrigeration system with high speed rotary pressure exchanger
US12007154B2 (en) 2021-06-09 2024-06-11 Energy Recovery, Inc. Heat pump systems with pressure exchangers

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4378681A (en) * 1981-09-08 1983-04-05 Modisette, Inc. Refrigeration system
JPS58104767A (ja) * 1981-12-16 1983-06-22 Matsushita Electric Ind Co Ltd 磁性流動体記録装置
JPS6176800A (ja) * 1984-09-25 1986-04-19 Sakou Giken:Kk 蒸気エゼクタ−
US6138456A (en) * 1999-06-07 2000-10-31 The George Washington University Pressure exchanging ejector and methods of use
JP5182159B2 (ja) * 2009-03-06 2013-04-10 株式会社デンソー エジェクタ方式の減圧装置およびこれを備えた冷凍サイクル
WO2013002872A2 (en) * 2011-06-10 2013-01-03 Carrier Corporation Ejector with motive flow swirl

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150285271A1 (en) * 2014-04-04 2015-10-08 Caltec Limited Jet pump
US20220290694A1 (en) * 2019-08-19 2022-09-15 Q.E.D. Environmental Systems, Inc. Pneumatic fluid pump with dual rotational swirling cleaning action
US20210348810A1 (en) * 2020-05-06 2021-11-11 Carrier Corporation Ejector refrigeration circuit
US20220307733A1 (en) * 2020-07-10 2022-09-29 Energy Recovery, Inc. Low energy consumption refrigeration system with a rotary pressure exchanger replacing the bulk flow compressor and the high pressure expansion system
US11982481B2 (en) 2020-07-10 2024-05-14 Energy Recovery, Inc. Refrigeration system with high speed rotary pressure exchanger
US12007154B2 (en) 2021-06-09 2024-06-11 Energy Recovery, Inc. Heat pump systems with pressure exchangers
US12085324B2 (en) 2021-06-09 2024-09-10 Energy Recovery, Inc. Refrigeration and heat pump systems with pressure exchangers

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JP2014224626A (ja) 2014-12-04

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